Total Impulse Measuring System for Solid Propellant Rocket Engine: Phase II Report
ROCKETDYNE CANOGA PARK CA
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Discussion and results of the two main considerations comprising the intermediate Phase II effort are presented 1 fabrication and test of the component parts of the system prior to their inclusion in the system and 2 assembly and test of the complete measurement system prior to its delivery to EAFB. Specific results of these separate but related program efforts are, respectively 1 source inspections and tests, where needed, to determine compliance with Rocketdyne drawings and specifications, and 2 alignment measurements and detailed tests to determine that the overall system peerformance conformed to the contractual requirement of 0.1 accuracy.
- Solid Propellant Rocket Engines